Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure
In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Hirwani, Chetan Kumar [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2018transfer abstract |
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| Umfang: |
16 |
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| Übergeordnetes Werk: |
Enthalten in: Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy - Chang, Guanru ELSEVIER, 2015, Amsterdam [u.a.] |
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| Übergeordnetes Werk: |
volume:159 ; year:2018 ; day:1 ; month:07 ; pages:237-252 ; extent:16 |
| Links: |
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| DOI / URN: |
10.1016/j.oceaneng.2018.04.035 |
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ELV043103324 |
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| 520 | |a In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. | ||
| 520 | |a In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. | ||
| 650 | 7 | |a Experimental validation |2 Elsevier | |
| 650 | 7 | |a Delaminated composite panel |2 Elsevier | |
| 650 | 7 | |a Nonlinear bending |2 Elsevier | |
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10.1016/j.oceaneng.2018.04.035 doi GBV00000000000487.pica (DE-627)ELV043103324 (ELSEVIER)S0029-8018(18)30489-X DE-627 ger DE-627 rakwb eng 540 VZ 660 VZ 540 VZ BIODIV DE-30 fid 42.13 bkl Hirwani, Chetan Kumar verfasserin aut Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure 2018transfer abstract 16 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. Experimental validation Elsevier Delaminated composite panel Elsevier Nonlinear bending Elsevier Mechanical load Elsevier HOST Elsevier Panda, Subrata Kumar oth Enthalten in Elsevier Science Chang, Guanru ELSEVIER Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy 2015 Amsterdam [u.a.] (DE-627)ELV01276728X volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 https://doi.org/10.1016/j.oceaneng.2018.04.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U FID-BIODIV SSG-OLC-PHA 42.13 Molekularbiologie VZ AR 159 2018 1 0701 237-252 16 |
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10.1016/j.oceaneng.2018.04.035 doi GBV00000000000487.pica (DE-627)ELV043103324 (ELSEVIER)S0029-8018(18)30489-X DE-627 ger DE-627 rakwb eng 540 VZ 660 VZ 540 VZ BIODIV DE-30 fid 42.13 bkl Hirwani, Chetan Kumar verfasserin aut Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure 2018transfer abstract 16 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. Experimental validation Elsevier Delaminated composite panel Elsevier Nonlinear bending Elsevier Mechanical load Elsevier HOST Elsevier Panda, Subrata Kumar oth Enthalten in Elsevier Science Chang, Guanru ELSEVIER Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy 2015 Amsterdam [u.a.] (DE-627)ELV01276728X volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 https://doi.org/10.1016/j.oceaneng.2018.04.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U FID-BIODIV SSG-OLC-PHA 42.13 Molekularbiologie VZ AR 159 2018 1 0701 237-252 16 |
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10.1016/j.oceaneng.2018.04.035 doi GBV00000000000487.pica (DE-627)ELV043103324 (ELSEVIER)S0029-8018(18)30489-X DE-627 ger DE-627 rakwb eng 540 VZ 660 VZ 540 VZ BIODIV DE-30 fid 42.13 bkl Hirwani, Chetan Kumar verfasserin aut Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure 2018transfer abstract 16 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. Experimental validation Elsevier Delaminated composite panel Elsevier Nonlinear bending Elsevier Mechanical load Elsevier HOST Elsevier Panda, Subrata Kumar oth Enthalten in Elsevier Science Chang, Guanru ELSEVIER Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy 2015 Amsterdam [u.a.] (DE-627)ELV01276728X volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 https://doi.org/10.1016/j.oceaneng.2018.04.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U FID-BIODIV SSG-OLC-PHA 42.13 Molekularbiologie VZ AR 159 2018 1 0701 237-252 16 |
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10.1016/j.oceaneng.2018.04.035 doi GBV00000000000487.pica (DE-627)ELV043103324 (ELSEVIER)S0029-8018(18)30489-X DE-627 ger DE-627 rakwb eng 540 VZ 660 VZ 540 VZ BIODIV DE-30 fid 42.13 bkl Hirwani, Chetan Kumar verfasserin aut Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure 2018transfer abstract 16 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. Experimental validation Elsevier Delaminated composite panel Elsevier Nonlinear bending Elsevier Mechanical load Elsevier HOST Elsevier Panda, Subrata Kumar oth Enthalten in Elsevier Science Chang, Guanru ELSEVIER Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy 2015 Amsterdam [u.a.] (DE-627)ELV01276728X volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 https://doi.org/10.1016/j.oceaneng.2018.04.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U FID-BIODIV SSG-OLC-PHA 42.13 Molekularbiologie VZ AR 159 2018 1 0701 237-252 16 |
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10.1016/j.oceaneng.2018.04.035 doi GBV00000000000487.pica (DE-627)ELV043103324 (ELSEVIER)S0029-8018(18)30489-X DE-627 ger DE-627 rakwb eng 540 VZ 660 VZ 540 VZ BIODIV DE-30 fid 42.13 bkl Hirwani, Chetan Kumar verfasserin aut Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure 2018transfer abstract 16 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. Experimental validation Elsevier Delaminated composite panel Elsevier Nonlinear bending Elsevier Mechanical load Elsevier HOST Elsevier Panda, Subrata Kumar oth Enthalten in Elsevier Science Chang, Guanru ELSEVIER Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy 2015 Amsterdam [u.a.] (DE-627)ELV01276728X volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 https://doi.org/10.1016/j.oceaneng.2018.04.035 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U FID-BIODIV SSG-OLC-PHA 42.13 Molekularbiologie VZ AR 159 2018 1 0701 237-252 16 |
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Enthalten in Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy Amsterdam [u.a.] volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 |
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Enthalten in Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy Amsterdam [u.a.] volume:159 year:2018 day:1 month:07 pages:237-252 extent:16 |
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Self-healable hydrogel on tumor cell as drug delivery system for localized and effective therapy |
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Numerical and experimental validation of nonlinear deflection and stress responses of pre-damaged glass-fibre reinforced composite structure |
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In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. |
| abstractGer |
In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. |
| abstract_unstemmed |
In the present article, nonlinear static deflections of internally damaged shear deformable laminated composite curved (single and doubly) shell panel are investigated numerically under the quasi-static loading and validated with experimental results. For the numerical analysis, a general nonlinear mathematical model of the laminated composite curved shell panel including the effect of the internal damage is derived with the help of two higher-order kinematic theories and Green-Lagrange nonlinear strain. The desired governing equation is obtained by minimizing the energy expression and solved via nonlinear finite element steps. The numerical responses are computed via a generic MATLAB code developed based on the present mathematical formulation. The degree of accuracy of the current numerical model has been checked and the subsequent validation is established by comparing the present results with available published results. In addition, an experimental investigation has also been carried out for the comparison purpose via three-point bend test on the laminated Glass/Epoxy composite with artificial delamination. Lastly, numbers of numerical examples are solved to demonstrate the implicit behavior of the currently developed higher-order nonlinear model for the analysis of the pre-damaged layered structure. |
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